28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-4.3.3

INTERDISCIPLINARY COMPLEX DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES

M. J. Ivanov, S. V. Kharkovsky, L. A. Magerramova, R. Z. Nigmatullin, V. D. Venediktov
CIAM, Russian Federation

Keywords: turbine, optimization, cooling scheme

This paper presents unified interdisciplinary mathematical models of gas dynamic, heat transfer and heat conductivity, strength and vibration processes, which takes place in high and low pressure turbines of modern aircraft engines. These models are relevant to high class models based on real 3D geometry of turbines.

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